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首页|期刊导航|航空材料学报|原位纳米Al-O结构增强Al基复合材料的显微组织和拉伸性能

原位纳米Al-O结构增强Al基复合材料的显微组织和拉伸性能

张涛 张良贤 匡蜀黔 姜腾蛟 赵科 刘金铃

航空材料学报2025,Vol.45Issue(6):101-108,8.
航空材料学报2025,Vol.45Issue(6):101-108,8.DOI:10.11868/j.issn.1005-5053.2025.000052

原位纳米Al-O结构增强Al基复合材料的显微组织和拉伸性能

Microstructure and tensile properties of in-situ nano-Al-O reinforced Al matrix composites

张涛 1张良贤 1匡蜀黔 1姜腾蛟 1赵科 2刘金铃1

作者信息

  • 1. 西南交通大学力学与航空航天学院,成都 611756||西南交通大学先进结构材料力学行为与服役安全四川省重点实验室,成都 611756
  • 2. 四川轻化工大学材料科学与工程学院,四川 自贡 643000
  • 折叠

摘要

Abstract

In-situ nano-Al-O reinforced aluminum matrix composites are fabricated via the powder hot extrusion method,and their distinctive microstructural attributes are examined to ascertain their impact on the room temperature tensile properties of these composites.Microstructural observations and mechanical property evaluations are conducted utilizing advanced characterization techniques,including X-ray diffraction(XRD),scanning electron microscopy(SEM),and transmission electron microscopy(TEM),alongside room temperature tensile testing.The findings reveal that numerous in-situ formed nano-Al-O structures are uniformly dispersed throughout the fine-grained aluminum matrix,with grain sizes approximately 500 nm.Some of these nanostructures exhibit strip-like morphologies,possessing an average width of 20 nm and length of 65 nm,while others display short rod-like morphologies,with an average width of 10 nm and length of 20 nm.Attributable to the reinforcing effect of the nano-Al-O structures,the room temperature yield strength and ultimate tensile strength of the aluminum matrix composites attain 402 MPa and 494 MPa,respectively,marking a significant increase of 2.90 times and 2.66 times compared to pure aluminum(103 MPa and 135 MPa,respectively).Notably,these composites maintain ductile fracture characteristics.

关键词

铝基复合材料/粉末热挤压/Al-O结构/力学性能

Key words

aluminum matrix composite/powder hot extrusion/Al-O structure/mechanical property

分类

航空航天

引用本文复制引用

张涛,张良贤,匡蜀黔,姜腾蛟,赵科,刘金铃..原位纳米Al-O结构增强Al基复合材料的显微组织和拉伸性能[J].航空材料学报,2025,45(6):101-108,8.

基金项目

四川省科技计划重点研发项目(2020YFG0140) (2020YFG0140)

航空材料学报

OA北大核心

1005-5053

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